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Ace VTOL · Australia
GT Slipstream
Ace VTOL GT Slipstream
矢量推力 · 概念设计 · 核查 2026-10-01
下列为 VFS 目录披露的参数,包含设计目标及历史版本信息。目录阶段不等于适航或量产状态;不同任务条件的航程与载荷不能直接当作同一条件下的性能。
主要参数
- 座位/载员
- 2 passengers
- 乘客
- 未公开/未录入
- 驾驶方式
- Low earth orbit satellite-hosted blockchain and AI flight management system with a virtual reality pilot interface
- 航程(按来源口径)
- 未公开/未录入
- 巡航速度
- 未公开/未录入
- 最大速度
- 未公开/未录入
- 最大起飞重量
- 未公开/未录入
- 载荷
- 未公开/未录入
- 空重
- 未公开/未录入
- 长度
- 未公开/未录入
- 翼展
- 未公开/未录入
- 高度
- 未公开/未录入
- 动力来源
- Batteries with 8 second recharging or hybrid-electric using hydrogen fuel cells. Uses atmospheric ion in-flight recharging.
- 电机
- 12 electric motors
- 旋翼/螺旋桨
- 4 next gen plasma engines
- 续航时间
- 未公开/未录入
- 飞行高度
- 未公开/未录入
- 安全设计
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. The aircraft has a three stage safety redundancy built into its systems.
全部原始参数
Specifications:
- Aircraft type
- eVTOL or hybrid-electric VTOL passenger and cargo concept design aircraft
- Piloting
- Low earth orbit satellite-hosted blockchain and AI flight management system with a virtual reality pilot interface
- Capacity
- 2 passengers
- Propellers
- 4 next gen plasma engines
- Electric motors
- 12 electric motors
- Power source
- Batteries with 8 second recharging or hybrid-electric using hydrogen fuel cells. Uses atmospheric ion in-flight recharging.
- Fuselage
- Carbon fiber composite
- Window
- Canopy over cockpit
- Landing gear
- Retractable quadricycle strut landing gear
- Safety features
- Distributed Electric Propulsion (DEP), provides safety through redundancy for its passengers and/or cargo. DEP means having multiple propellers (or ducted fans) and motors on the aircraft so if one or more propellers (ducted fans) or motors fail, the other working propellers (or ducted fans) and motors can safely land the aircraft. The aircraft has a three stage safety redundancy built into its systems.